gptkbp:instance_of
|
gptkb:helicopter
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gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Mi-26
|
gptkbp:aircraft_operated
|
gptkb:helicopter
|
gptkbp:armament
|
gptkb:none
|
gptkbp:combat_role
|
transporting troops and equipment
|
gptkbp:crew
|
gptkb:5
|
gptkbp:design
|
gptkb:Mikhail_Mil
|
gptkbp:diameter
|
32 m
|
gptkbp:ecological_role
|
operates in extreme conditions
|
gptkbp:elevation
|
4,600 m
|
gptkbp:emergency_services
|
dual engine redundancy
|
gptkbp:engine_type
|
turbo-shaft
|
gptkbp:exported_to
|
several countries
|
gptkbp:features
|
twin rotor system
|
gptkbp:first_flight
|
gptkb:1977
|
gptkbp:fuel_capacity
|
3,000 L
|
gptkbp:historical_significance
|
first helicopter to lift 20 tons
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mi-26 A
|
gptkbp:interior_features
|
flexible cargo space
|
gptkbp:introduced
|
gptkb:1980
|
gptkbp:is_used_by
|
gptkb:Russian_Armed_Forces
|
gptkbp:length
|
40 m
|
gptkbp:maintenance
|
requires specialized facilities
|
gptkbp:manufacturer
|
gptkb:Mil_Moscow_Helicopter_Plant
|
gptkbp:max_speed
|
295 km/h
|
gptkbp:max_takeoff_weight
|
800 m
1,000 m
56,000 kg
|
gptkbp:military_technology
|
cargo transport
|
gptkbp:notable_event
|
used in disaster relief
|
gptkbp:notable_features
|
largest helicopter in the world
|
gptkbp:notable_users
|
India, Ukraine
|
gptkbp:number_built
|
over 300
|
gptkbp:operational_history
|
used in various conflicts
|
gptkbp:operational_range
|
1,000 km
|
gptkbp:operational_status
|
active
|
gptkbp:origin
|
gptkb:Monarch
|
gptkbp:power_output
|
11,400 hp
|
gptkbp:primary_user
|
gptkb:Russia
|
gptkbp:production_years
|
gptkb:1980
present
|
gptkbp:range
|
800 km
|
gptkbp:role
|
transport helicopter
|
gptkbp:safety_features
|
high
|
gptkbp:seating_capacity
|
90
20,000 kg
large cargo doors
|
gptkbp:service_ceiling
|
4,600 m
|
gptkbp:services
|
gptkb:1983
|
gptkbp:training
|
pilot training necessary
|
gptkbp:type
|
heavy-lift helicopter
|
gptkbp:variant
|
gptkb:Mi-26
Mi-26 T, Mi-26 TP
|
gptkbp:wingspan
|
32 m
|